EP3623288B8 - Aéronef à décollage et atterrissage verticaux (adav) doté d'une commande de positionnement de rotor de croisière pour une traînée minimale - Google Patents

Aéronef à décollage et atterrissage verticaux (adav) doté d'une commande de positionnement de rotor de croisière pour une traînée minimale Download PDF

Info

Publication number
EP3623288B8
EP3623288B8 EP19196695.1A EP19196695A EP3623288B8 EP 3623288 B8 EP3623288 B8 EP 3623288B8 EP 19196695 A EP19196695 A EP 19196695A EP 3623288 B8 EP3623288 B8 EP 3623288B8
Authority
EP
European Patent Office
Prior art keywords
vtol
landing
aircraft
positioning control
vertical take
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP19196695.1A
Other languages
German (de)
English (en)
Other versions
EP3623288B1 (fr
EP3623288A1 (fr
Inventor
Júlio Cesar Graves
Yasser Mahmud Abdallah
Leandro Guimarães Maia
Carlos Eduardo Vieira de Souza
Luiz Felipe Ribeiro Valentini
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Eve Uam LLC
Original Assignee
Eve Uam LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eve Uam LLC filed Critical Eve Uam LLC
Publication of EP3623288A1 publication Critical patent/EP3623288A1/fr
Publication of EP3623288B1 publication Critical patent/EP3623288B1/fr
Application granted granted Critical
Publication of EP3623288B8 publication Critical patent/EP3623288B8/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/30—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with provision for reducing drag of inoperative rotor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/68—Transmitting means, e.g. interrelated with initiating means or means acting on blades using electrical energy, e.g. having electrical power amplification
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Retarders (AREA)
  • Epoxy Compounds (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
EP19196695.1A 2018-09-11 2019-09-11 Aéronef à décollage et atterrissage verticaux (adav) doté d'une commande de positionnement de rotor de croisière pour une traînée minimale Active EP3623288B8 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US201862729603P 2018-09-11 2018-09-11

Publications (3)

Publication Number Publication Date
EP3623288A1 EP3623288A1 (fr) 2020-03-18
EP3623288B1 EP3623288B1 (fr) 2022-03-16
EP3623288B8 true EP3623288B8 (fr) 2022-04-27

Family

ID=67928706

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19196695.1A Active EP3623288B8 (fr) 2018-09-11 2019-09-11 Aéronef à décollage et atterrissage verticaux (adav) doté d'une commande de positionnement de rotor de croisière pour une traînée minimale

Country Status (4)

Country Link
US (1) US11708157B2 (fr)
EP (1) EP3623288B8 (fr)
CN (1) CN110884652B (fr)
BR (1) BR102019018805A8 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11332239B2 (en) * 2017-07-06 2022-05-17 Shanghai Autoflight Co., Ltd. Fixed-wing VTOL aerial vehicle
FR3078945B1 (fr) * 2018-03-13 2022-05-06 Innostar Aerodyne hybride de type vtol ou stol (basculement rotor)
US20230257112A1 (en) * 2019-02-28 2023-08-17 Beta Air, Llc Vertical take-off and landing (vtol) aircraft
USD914171S1 (en) * 2019-05-10 2021-03-23 Embraer S.A. Vertical take-off and landing craft
IL278514A (en) * 2020-11-05 2022-06-01 Gadfin Ltd An optimization system based on an aircraft and a method for it
US11840351B2 (en) * 2021-04-05 2023-12-12 Beta Air, Llc Aircraft for self-neutralizing flight
US11365001B1 (en) 2021-06-29 2022-06-21 Beta Air, Llc Method of propulsor management in electric aircraft
CN113277076B (zh) * 2021-07-22 2021-10-08 国网通用航空有限公司 垂直起降固定翼无人机螺旋桨减阻装置及其控制方法
US11377201B1 (en) * 2021-07-23 2022-07-05 Beta Air, Llc System and method for flight control of an electric vertical takeoff and landing aircraft
US11702200B1 (en) * 2021-12-29 2023-07-18 Beta Air, Llc System for a vertical takeoff and landing aircraft with an in-boom lift propulsor
JP2024051713A (ja) 2022-09-30 2024-04-11 本田技研工業株式会社 航空機の制御装置

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110001020A1 (en) * 2009-07-02 2011-01-06 Pavol Forgac Quad tilt rotor aerial vehicle with stoppable rotors
TWI538852B (zh) 2011-07-19 2016-06-21 季航空股份有限公司 個人飛機
US9120560B1 (en) 2011-10-13 2015-09-01 Latitude Engineering, LLC Vertical take-off and landing aircraft
EP2604519A4 (fr) 2011-10-17 2015-07-15 Yuneec Technology Co Limited Avion composite constitué d'une voilure fixe et d'hélices à commande électrique
CN202728575U (zh) * 2011-10-17 2013-02-13 田瑜 固定翼与电动多旋翼组成的复合飞行器
CN103043212B (zh) * 2011-10-17 2016-06-08 优利科技有限公司 固定翼与电动多旋翼组成的复合飞行器
US20130092799A1 (en) * 2011-10-17 2013-04-18 Yu Tian Fixed-wing and electric multi-rotor composite aircraft
US9527581B2 (en) * 2013-07-25 2016-12-27 Joby Aviation, Inc. Aerodynamically efficient lightweight vertical take-off and landing aircraft with multi-configuration wing tip mounted rotors
DE102013109392A1 (de) * 2013-08-29 2015-03-05 Airbus Defence and Space GmbH Schnellfliegendes, senkrechtstartfähiges Fluggerät
WO2015157114A1 (fr) 2014-04-11 2015-10-15 Sada-Salinas Jaime G Nacelles modulaires permettant des capacités de décollage et d'atterrissage verticaux (vtol) des véhicules aériens à ailes fixes et des systèmes et procédés associés
US9334049B1 (en) * 2014-12-03 2016-05-10 Amazon Technologies, Inc. Single blade rotor system for use in a vertical takeoff and landing (VTOL) aircraft
CN106143878A (zh) * 2015-03-27 2016-11-23 中国矿业大学徐海学院 基于滑模控制算法的多轴固定翼一体机控制器
CN105059541A (zh) * 2015-08-21 2015-11-18 符星 一种新型多轴无人机
US10183744B2 (en) 2016-02-10 2019-01-22 Lockheed Martin Corporation Magnetic orientation detent
US9944387B2 (en) 2016-05-24 2018-04-17 Kitty Hawk Corporation Stopped rotor aircraft
US10364036B2 (en) * 2016-10-18 2019-07-30 Kitty Hawk Corporation Multicopter with boom-mounted rotors
EP3532376A1 (fr) * 2016-10-31 2019-09-04 LORD Corporation Systèmes et procédés de détection intelligents intégrés
US10479496B2 (en) * 2016-10-31 2019-11-19 Lockheed Martin Corporation Magnetic orientation detent with motor assist
CN107200123B (zh) * 2017-04-21 2019-09-06 北京航空航天大学 一种复合式飞行器中多旋翼电动螺旋桨顺桨方式的控制系统及方法
US10053213B1 (en) * 2017-05-08 2018-08-21 Pinnacle Vista, LLC Multi-copter lift body aircraft with tail pusher
WO2019084487A1 (fr) * 2017-10-27 2019-05-02 Elroy Air, Inc. Aéronef multicoptère composite
CN108001679A (zh) * 2017-11-30 2018-05-08 湖北航天飞行器研究所 三涵道螺旋桨动力方式的可垂直起降固定翼无人飞行器

Also Published As

Publication number Publication date
EP3623288B1 (fr) 2022-03-16
US20200079501A1 (en) 2020-03-12
EP3623288A1 (fr) 2020-03-18
BR102019018805A8 (pt) 2023-01-10
US11708157B2 (en) 2023-07-25
BR102019018805A2 (pt) 2020-07-28
CN110884652B (zh) 2024-05-10
CN110884652A (zh) 2020-03-17

Similar Documents

Publication Publication Date Title
EP3623288B8 (fr) Aéronef à décollage et atterrissage verticaux (adav) doté d'une commande de positionnement de rotor de croisière pour une traînée minimale
EP3724071A4 (fr) Système d'aéronef à décollage et atterrissage verticaux (vtol) à géométrie variable
EP3684687A4 (fr) Système d'actionnement d'inclinaison pour aéronef à décollage et atterrissage verticaux (adav)
EP3676679A4 (fr) Commandes manuelles découplées pour aéronef ayant des capacités de décollage et d'atterrissage verticaux et de vol vers l'avant
WO2016003530A3 (fr) Véhicule aérien sans pilote (uav) de type à décollage et atterrissage verticaux (adav)
EP3941828A4 (fr) Aéronef à décollage et atterrissage verticaux (vtol)
WO2016053739A3 (fr) Commande de position de fuselage avant d'un aéronef à voilure tournante
EP3746745A4 (fr) Procédés et systèmes de détermination de plans de vol pour véhicules aériens à décollage et atterrissage verticaux (vtol)
EP3335989A4 (fr) Aéronef à voilure fixe capable de décoller et d'atterrir verticalement, et son procédé de commande de pilotage
EP3458356A4 (fr) Aéronef à décollage et atterrissage verticaux à configurations d'ailes inclinées
WO2016200502A3 (fr) Aéronef vtol modulaire commandé à distance et système reconfigurable utilisant celui-ci
WO2016109003A3 (fr) Fuselage delta pour aéronef à décollage et atterrissage verticaux (vtol)
WO2017131834A3 (fr) Système à ailes pivotantes destiné à un avion adav
EP3878752A4 (fr) Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé
WO2016028358A3 (fr) Aéronef vtol à hautes performances
EP3583027A4 (fr) Aéronef léger à décollage et atterrissage verticaux
EP4026770A4 (fr) Système d'atterrissage automatique pour aéronef à décollage/atterrissage vertical, aéronef à décollage/atterrissage vertical et procédé de commande pour l'atterrissage d'un aéronef à décollage/atterrissage vertical
SG11202008018XA (en) Fixed-wing unmanned aerial vehicle take-off and landing system and method thereof
EP3609783A4 (fr) Aéronef à décollage et atterrissage verticaux
EP3746361A4 (fr) Procédés et systèmes de décollage et d'atterrissage écoénergétiques pour véhicules aériens à décollage et atterrissage verticaux (vtol)
EP3668792A4 (fr) Procédés et systèmes pour améliorer la précision des atterrissages autonomes d'aéronefs de type drone sur des cibles d'atterrissage
EP4085005A4 (fr) Aéronef à hélices positionnées en bout d'aile
RU2014119525A (ru) Вертоплан - скоростной винтокрылый летательный аппарат
IL287462A (en) An air vehicle for vertical takeoff and landing and a method of control
EP3674212A4 (fr) Procédé de vol à grande vitesse et aéronef à voilure annulaire

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RIN1 Information on inventor provided before grant (corrected)

Inventor name: MAIA, LEANDRO GUIMARAES

Inventor name: VALENTINI, LUIZ FELIPE RIBEIRO

Inventor name: ABDALLAH, YASSER MAHMUD

Inventor name: VIEIRA DE SOUZA, CARLOS EDUARDO

Inventor name: GRAVES, JULIO CESAR

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20200918

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20210310

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20211117

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: PK

Free format text: BERICHTIGUNG B8

Ref country code: CH

Ref legal event code: EP

Ref country code: DE

Ref legal event code: R096

Ref document number: 602019012543

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1475706

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220415

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: EVE UAM, LLC

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602019012543

Country of ref document: DE

Owner name: EVE UAM, LLC, WILMINGTON, US

Free format text: FORMER OWNER: EMBRAER S.A., SAO JOSE DOS CAMPOS, SAO PAULO, BR

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20220316

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220616

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220616

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1475706

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220316

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220617

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220718

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220716

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602019012543

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

26N No opposition filed

Effective date: 20221219

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20220930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220930

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220911

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220930

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20230907

Year of fee payment: 5

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20230911

Year of fee payment: 5

Ref country code: DE

Payment date: 20230929

Year of fee payment: 5

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20190911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220316